Spatial vibration protection in a turbopump of hydrogen rocket engines
- Autores: Belousov A.I.1, Ponomarev Y.K.1
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Afiliações:
- Samara University
- Edição: Volume 59, Nº 3 (2016)
- Páginas: 388-394
- Seção: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229791
- DOI: https://doi.org/10.3103/S1068799816030156
- ID: 229791
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Resumo
We discuss the use of multilayered annular-plate dampers as rotor supports in turbopumps of the RD-0120 and RD-0146 rocket engines. We present a technique of calculating the elastic and damping characteristics of multilayer corrugated annular supports in the case of the conical precession of the rotor.
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Sobre autores
A. Belousov
Samara University
Autor responsável pela correspondência
Email: aibelousov@mail.ru
Rússia, shosse Moskovskoe 34, Samara, 443086
Yu. Ponomarev
Samara University
Email: aibelousov@mail.ru
Rússia, shosse Moskovskoe 34, Samara, 443086
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